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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Shakeri, M.
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Topics
Publications (12/12 displayed)
- 2018Free vibration analysis and design optimization of SMA/Graphite/Epoxy composite shells in thermal environmentscitations
- 2016Modeling and analysis of reversible shape memory adaptive panelscitations
- 2015Micro-mechanics of composite with SMA fibers embedded in metallic/polymeric matrix under off-axial loadingscitations
- 2015A simple and efficient 1-D macroscopic model for shape memory alloys considering ferro-elasticity effect
- 2015Micromechanics of shape memory alloy fiber-reinforced composites subjected to multi-axial non-proportional loadingscitations
- 2015Micro-macro thermo-mechanical analysis of axisymmetric shape memory alloy composite cylinderscitations
- 2014Shape control of shape memory alloy composite beams in the post-buckling regimecitations
- 2014Active shape/stress control of shape memory alloy laminated beamscitations
- 2014On the vibration control capability of shape memory alloy composite beamscitations
- 2014A robust three-dimensional phenomenological model for polycrystalline SMAscitations
- 2013An Investigation on Low Velocity Impact Response of Multilayer Sandwich Composite Structurescitations
- 2013A phenomenological SMA model for combined axial-torsional proportional/non-proportional loading conditionscitations
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article
On the vibration control capability of shape memory alloy composite beams
Abstract
<p>In this paper, the vibration control capability of shape memory alloy (SMA) composite beams subjected to impulsive loads is examined. In order to simulate the SMA response, a one-dimensional constitutive model is introduced which is able to reproduce pseudo-elasticity, martensite transformation/orientation and in particular ferro-elasticity effects. A numerical algorithm is presented to solve non-linear SMA constitutive model by means of an elastic-predictor inelastic-corrector return map procedure. The equivalent single layer theory of Rayleigh-Euler-Bernoulli is used to describe displacement field of SMA laminated composite beams. Geometrical non-linearity is also considered in the von Karman sense. Considering rotary inertia effects, finite element equations of motion are developed using the Hamilton principle. Newmark and Newton-Raphson methods are utilized to obtain an incremental solution of the problem. Extensive numerical results are presented to provide an insight into the influence of pre-strain, temperature, location and thickness of SMA layers on the vibration control of SMA composite beams subjected to various blast pulses. Considering ferro-elasticity effect, results reveal the fact that SMA layers with high pre-strain have a passive vibration control capability in low temperatures and yield a better efficiency in comparison with pseudo-elastic SMA layers.</p>